EP3080447A1 - Unité de décharge de pale de rotor pour éoliennes - Google Patents

Unité de décharge de pale de rotor pour éoliennes

Info

Publication number
EP3080447A1
EP3080447A1 EP14811760.9A EP14811760A EP3080447A1 EP 3080447 A1 EP3080447 A1 EP 3080447A1 EP 14811760 A EP14811760 A EP 14811760A EP 3080447 A1 EP3080447 A1 EP 3080447A1
Authority
EP
European Patent Office
Prior art keywords
rotor
blade
discharge unit
conductive
slideway
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
EP14811760.9A
Other languages
German (de)
English (en)
Other versions
EP3080447B1 (fr
Inventor
Torben Friis Baun
Anders Niels Hansen
Claus Grøn LYNGBY
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Vestas Wind Systems AS
Original Assignee
Vestas Wind Systems AS
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Priority claimed from GB201321695A external-priority patent/GB201321695D0/en
Application filed by Vestas Wind Systems AS filed Critical Vestas Wind Systems AS
Publication of EP3080447A1 publication Critical patent/EP3080447A1/fr
Application granted granted Critical
Publication of EP3080447B1 publication Critical patent/EP3080447B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03D—WIND MOTORS
    • F03D80/00—Details, components or accessories not provided for in groups F03D1/00 - F03D17/00
    • F03D80/30—Lightning protection
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2260/00—Function
    • F05B2260/50—Kinematic linkage, i.e. transmission of position
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00—Energy generation through renewable energy sources
    • Y02E10/70—Wind energy
    • Y02E10/72—Wind turbines with rotation axis in wind direction

Definitions

  • the invention relates to a rotor-blade discharge unit of a wind turbine, enabling electric charges to be discharged from a rotor blade, and to a wind turbine comprising one or more rotor-blade discharge units for each rotor blade of the wind turbine.
  • Known lightning conductor systems for wind turbines enable electric charges to be discharged from the rotor blades.
  • a gap in the lightning down-conductor between a pitchable rotor blade and the wind turbine's nacelle is bridged by a lightning current transfer arrangement having sliding contacts which contact complementary slideways.
  • the sliding contacts include a contact rod which provides the electric contact with the slideway, and a slide pad surrounding the contact rod to increase the sliding surface and lower sliding friction.
  • a rotor-blade discharge unit enabling electric charges to be discharged from a rotor blade of a wind turbine is provided.
  • the rotor-blade discharge unit comprises at least one current transfer arrangement.
  • Each current transfer arrangement comprises a roller device, an electrically conductive slideway, and a spark gap.
  • the roller device is biased towards the conductive slideway and is movable relative to the conductive slideway.
  • the roller device comprises at least one contact wheel having a rolling surface.
  • the contact wheel is arranged to roll on the conductive slideway and is biased towards the conductive slideway, wherein the rolling surface is arranged to deform against the conductive slideway under the bias acting on the roller device. Thereby a contact surface is formed between the wheel and the conductive slideway.
  • a first current path to discharge electric charges is formed by the contact wheel and the conductive slideway, which is in contact with the contact wheel.
  • a second current path is formed by a spark gap if a spark bridges that spark gap.
  • This second current path is connected in parallel to the first current path.
  • a wind turbine comprising a nacelle, a hub, at least one rotor blade, and at least one rotor-blade discharge unit enabling electric charges to be discharged from the at least one rotor blade.
  • the rotor-blade discharge unit comprises at least one current transfer arrangement.
  • Each current transfer arrangement comprises a roller device, an electrically conductive slideway, and a spark gap.
  • the roller device is biased towards the conductive slideway and is movable relative to the conductive slideway.
  • the roller device comprises at least one contact wheel having a rolling surface.
  • the contact wheel is arranged to roll on the conductive slideway and is biased towards the conductive slideway wherein the rolling surface is arranged to deform against the conductive slideway under the bias acting on the roller device. Thereby a contact surface between the wheel and the conductive slideway is formed.
  • a first current path to discharge electric charges is formed by the contact wheel and the conductive slideway, which is in contact with the contact wheel.
  • a second current path is formed by a spark gap if a spark bridges that spark gap. This second current path is connected in parallel to the first current path.
  • the at least one rotor-blade dis- charge unit enables electric charges originating from the at least one rotor blade to be discharged towards the nacelle.
  • the at least one rotor-blade discharge unit is mounted on the hub and is electrically insulated from the hub
  • Fig. 1 illustrates an embodiment of a wind turbine with a nacelle, a rotor with rotor blades, and a grounding system including a rotor blade discharge unit;
  • Fig. 2 illustrates an exemplary current transfer arrangement of the rotor blade discharge unit having a roller device with a chassis acting as a spark-gap electrode
  • Fig. 3 illustrates another exemplary current transfer arrangement having a roller device in which the spark-gap electrode is provided by a protrusion of the chassis;
  • Fig. 4 illustrates the hub portion of the wind turbine of Fig. 1 and a charge transfer region with an exemplary embodiment of a rotor-blade discharge unit;
  • Fig. 5 illustrates the charge transfer region with a first embodiment of a rotor-blade discharge unit oriented towards the rotor blade;
  • Fig. 6 illustrates the charge transfer region with a second embodiment of a rotor-blade discharge unit oriented towards the nacelle;
  • Fig. 7 illustrates the charge transfer region with a third embodiment of a rotor-blade discharge unit oriented both towards the rotor blade and the nacelle.
  • Fig. 1 illustrates an exemplary wind turbine with rotor blade discharge units.
  • a gap between a rotor blade and a nacelle, which are parts rotatable relative to each other, is bridged by a rotor-blade discharge unit that transfers an electric current arising from lightning striking a rotor blade directly from the root of that rotor blade to the nacelle.
  • a rotor-blade discharge unit that transfers an electric current arising from lightning striking a rotor blade directly from the root of that rotor blade to the nacelle.
  • static charges arising due to friction of the air with the rotor blades are discharged, as the rotor-blade discharge unit provides a permanent galvanic current path to ground potential.
  • the risk of contact-lift-off is reduced by the use of contact wheels arranged to deform against a conductive slideway under bias acting on the against the contact wheels.
  • the contact wheels may be made, at least at their rolling surface, of elastomeric electrically conductive or semi-conductive plastics, or of electrically conductive carbonaceous materials having a Shore D hardness of 18 or less.
  • the contact wheels elastically deform against a conductive slideway under bias acting on the contact wheels such that the contact area of the wheel against the conductive slideway is increased.
  • the rotor-blade discharge unit is arranged to provide electrical contact between conductive parts of the rotor blades of a wind turbine and a grounded part of the wind turbine, e.g. a slideway at the wind turbine's nacelle which, in turn, is connected to ground via the tower.
  • the rotor-blade discharge unit may comprise one or more current transfer arrangements.
  • a current transfer arrangement may comprise one or more roller devices, one or more electrically conductive slideways and one or more spark gaps.
  • a conductive slideway is mounted on a part of the wind turbine which is rotatable relative to another part of the wind turbine, e.g. a rotor blade of the wind turbine, a hub of the wind turbine or a nacelle of the wind turbine.
  • a conductive slideway may be mounted on a rotor blade and may be electrically connected to a rotor blade down conductor which may lead from a tip part of the rotor blade down to the conductive slideway.
  • Such a conductive slideway, mounted on a rotor blade is referred to as rotor-blade-side conductive slideway.
  • the tip part of the rotor blade may be equipped with a lightning receptor.
  • the rotor-blade-side conductive slideway is electrically connected to the rotor blade tip part.
  • a conductive slideway may be mounted on the nacelle of a wind turbine, referred to as nacelle-side conductive slideway.
  • the nacelle-side conductive slideway for example, is electrically connected to a grounded structural part of the nacelle. This structural part can be a main structure of the nacelle which is connected to a ground potential.
  • the roller device has one or more contact wheels which may be made of elastomeric electrically conductive or semi-conductive plastics at least in a region at the rolling surface.
  • the elastomeric semi-conductive plastics have resistivities of 10 "4 ⁇ -m - 100 kQ-m and elastomeric conductive plastics have resistivities of 10 ⁇ 6 ⁇ -m to 10 ⁇ 4 ⁇ -m.
  • elastomeric electrically conductive or semi-conductive plastics refers to conductive or semi-conductive solid plastic materials that are able to restore their original shape after a temporary deformation.
  • the elastomeric electrically conductive or semi-conductive plastic has a glass- transition temperature (where it loses most of its elasticity), for example, below minus 20°C, below minus 30°C, or below minus 4Q °C.
  • Elastomeric electrically conductive or semi-conductive plastics may be intrinsically electrically conductive or semi-conductive or may be intrinsically non-conductive elastomeric plastics made electrically conductive or semi-conductive by the addition of additives that provide the electrical conductivity, such as carbon black, graphite, carbon nanotubes, metal flakes, metal fibers, particles or fibers coated with metal, conductively coated minerals, conductively coated ceramics, pulverized anthracite, etc. Such additives may also be combined with intrinsically electrically conductive or semi-conductive elastomeric plastics to enhance the electrical conductivity. Furthermore, some intrinsically electrically non-conductive plastics can be made electrically conductive or semi-conductive by adding dopants, e.g. p-type dopants, such as Cl 2 , Br 2 , l 2 , BF 5 .
  • dopants e.g. p-type dopants, such as Cl 2 , Br 2 , l 2 , BF 5 .
  • Examples of intrinsically electrically conductive elastomeric plastics are polyaniline (PANI) and polypyrrole (PPy), an example for an intrinsically semi-conductive plastics is oxidized polyparaphenylene (PPP).
  • Polyacetylene (PAC) can be made electrically conductive by doping, for example, with p-type dopants.
  • Polyamide, polyoxymethylene (POMs), ultra high molecular weight polyethylene (UHMWPE), rubbers, such as polybutadiene rubber (PB) and styrene-butadiene rubber (SBR), and silicones (or siloxanes) are examples for elastomeric plastics which are intrinsically non-conductive and can be made conductive by additives, such as the above-mentioned ones.
  • Suitable electrically conductive carbonaceous materials having a Shore D hardness of 18 or less comprise mainly graphite. They may be fabricated by mixing graphite, one or more organic binders and one or more additives and then carbonizing the binder at high temperatures. Such materials are commercially available.
  • the one or more contact wheels of a roller device are arranged to move along a conductive slideway that may be mounted on a part of the wind turbine rotatable relative to the part on which the roller device is mounted.
  • the contact wheel(s) is (are) biased towards the conductive slideway. Owing to the elasticity of the contact wheel(s) an extended contact surface between the wheel and the conductive slideway is thereby formed, i.e. the wheels deform against the conductive slideway.
  • the current transfer arrangements also provide a spark gap between these two different parts of the wind turbine rotatable relative to each other. It therefore provides two parallel current paths.
  • the permanent galvanic current path enables static charges to be discharged from the rotor blades.
  • the other current path through the spark gap enables lightning current to be discharged.
  • the resistivity of the wheels will cause a voltage drop across the contact wheel(s) sufficient to fire a spark across the spark gap.
  • the lightning current will therefore bypass the contact wheel(s), thereby preventing any thermal damage to the contact wheel(s).
  • the first current path with permanent galvanic contact to discharge static electric charges is formed by the contact wheel(s) and the conductive slideway in contact with contact wheel(s).
  • the second current path provided to bypass the contact wheel(s) in the event of a lightning strike is formed between electrodes defining the spark gap.
  • the first and second current paths are electrically connected in parallel.
  • the roller device, or a part of it forms one of the electrodes of the spark-gap, and the other electrode of the spark gap is provided by the conductive slideway to which the roller device is biased.
  • the rotor-blade discharge unit is mounted on the hub by an elastically deformable strip.
  • the strip is made of electrically insulating material, e.g. a glass fibre/resin compound material, in order that the discharge current paths are electrically isolated from the hub.
  • the roller device has one, two, or more contact wheels.
  • the roller device has a chassis, and the contact wheels are rotatably mounted on the chassis.
  • the roller device is elastically biased towards the conductive slideway that forms a contact surface with the contact wheels mounted on the chassis of the roller device.
  • the bias is produced by an elastically deformable strip
  • one end of the strip is mounted on the hub and its other end is mounted on the roller device, thereby biasing the roller device towards the conductive slideway.
  • the roller device has only a single contact wheel. In other embodiments, it is equipped with two or more contact wheels.
  • the contact wheel(s) is (are), for example, rotatably mounted on the chassis by means of an axle (axles) arranged in axle bearings.
  • axle axle
  • One axle is equipped with a single contact wheel or, alternatively two or more contact wheels.
  • the contact wheels are successively arranged in the direction of travel.
  • the contact wheels are, for example, mounted on the leading part of the chassis on a front axle and at the trailing part of the chassis on a rear axle, thereby forming leading and trailing contact wheel(s).
  • the contact wheels may have a prolate shape (i.e. have an axial extension larger than the wheels diameter).
  • the slideway has the form of a planar circular ring; e.g. a slideway mounted on the face of the nacelle towards the hub.
  • the axles are oriented radially with respect to the circle center of the slideway to enable the contact wheel(s) to run along the circular slideway with reduced wear.
  • the contact wheels may have a conical shape, with the cone increasing in the radial direction of a circular slideway and a cone angle adapted to the curvature of the circular slideway so that the conical contact wheels run on the circular slideway without slip to reduce wear.
  • the chassis is hinged to the elastically bendable strips, e.g. by a swivel joint. This ensures that the bias produced by the force exerted by the bendable strip is distributed between the leading and trailing rollers, so that both rollers are equally urged towards the slideway and provide permanent gal- vanic contact.
  • the spark gap of a rotor-blade discharge unit is defined by an electrode that is electrically connected to the roller device but designed to be spatially separated from the roller device.
  • the current path, formed by the spark gap, upon occurrence of a spark bridging the spark gap, is therefore connected in parallel to the current path formed by the contact wheel(s) which is (are) in contact with the conductive slideway.
  • the roller(s) is (are) not thermally damaged by the lightning current, as the spark gap(s) is (are) spatially separated from the roller(s).
  • the chassis is arranged to move along the conductive slideway at a given distance by using contact wheel(s) that is (are) rotatably mounted on the chassis.
  • contact wheel(s) that is (are) rotatably mounted on the chassis.
  • a gap between the chassis and the conductive slideway is provided, thereby the chassis forms the spark gap electrode.
  • a frictionless movement in this context is defined to be a movement only hindered by rolling friction.
  • the spark-gap electrode is provided by one or more protrusions of the chassis, located on the surface of the chassis facing the conductive slideway.
  • the spark gap provides a current path, upon occurrence of a spark bridging the spark gap, i.e. the second current path connected in parallel to the first current path.
  • the chassis either acts as the spark-gap electrode itself or has a protrusion that acts as the spark-gap electrode, the second current path runs through the chassis.
  • the one or more contact wheels are mounted on the chassis in an electrically conducting manner, a current path may run from the contact wheels through the chassis, i.e. the first current path.
  • the wind turbine with a nacelle, a hub and one or more rotor blades is also equipped with one or more rotor-blade discharge units.
  • the nacelle is arranged to provide a nacelle-side conductive slideway as a part of the associated rotor-blade discharge unit and the one or more rotor blades are arranged to provide rotor-blade side conductive slideways as part of the associated rotor-blade discharge units.
  • a rotor-blade discharge unit may be mounted on the hub, in an electrically insulated manner, for example, using elastically bendable strips. In this way the rotor-blade discharge unit enables electric charges originating from the rotor blade(s) to be discharged onto the nacelle which, in turn, is electrically connected to the ground.
  • the electric charges are discharged from the rotor blades either by a combination of discharge cables and/or electrically conductive strips connected to a current transfer arrangement or by a plurality of current transfer arrangements connected by cables.
  • the one or more rotor blades of the wind turbine are arranged to be pitchable.
  • the one or more rotor-blade discharge units may be associated with the one or more rotor blades, thus the rotor blades are equipped with rotor-blade-side conductive slideways.
  • the roller-devices and corresponding contact wheels are biased towards the associated rotor- blade-side conductive slideways.
  • the roller device(s), as part of a current transfer arrangement establish the first and second current paths from the associated rotor blades to the hub.
  • the one or more rotor-blade discharge units thereby bypass pitch-bearings connecting the rotor blades to the hub that is electrically connected to a ground potential.
  • the rotor-blade discharge unit mounted on the hub, is arranged to be electrically connected to the nacelle by one or more roller devices.
  • the roller device(s), comprised by the current transfer arrangement, i.e. the rotor-blade discharge unit, are biased towards the nacelle-side conductive slideway, also comprised by the current transfer arrangement.
  • the electrical connection, leading charges from the rotor-blade(s) to the roller device is provided by a discharge cable, a conductive band, a conductive strip or the like.
  • the rotor-blade discharge units thereby bypass the main shaft-bearing connecting the hub to the nacelle.
  • a first and second current path from the nacelle to another part of the wind turbine that is rotatable relative to the nacelle is formed.
  • the one or more rotor-blade discharge units comprise more than one current transfer arrangement, wherein a first roller device, comprised by a first current transfer arrangement is biased towards a rotor-blade-side conductive slideway.
  • the contact wheels provide electrical contact between the roller device and this rotor-blade-side conductive slideway that may be connected to a rotor-blade down conductor which, in turn, may be connected to lightning receptors mounted on the rotor blade.
  • a second roller device, comprised by a second current-transfer arrangement is biased towards the nacelle-side conductive slideway connected to a ground potential.
  • the two current transfer arrangements are electrically connected, for example, by a discharge-cable, thereby enabling a transfer of charges from the rotor-blade-side conductive slideway to the nacelle-side conductive slideway over the first and second current path formed by the current transfer arrangements.
  • pitch bearings connecting the rotor blades to the hub and the main-shaft bearing connecting the hub to the nacelle are bypassed.
  • an exemplary wind turbine 1 has a rotor with a hub 4 rotatably connected to a nacelle 3 mounted on a yaw bearing on top of a tower 2.
  • the nacelle is electrically connected to the ground 12.
  • the rotor of the wind turbine 1 has three rotor blades 5 with a tip part 8, a lightning receptor 6 mounted on the tip part 8, and a rotor blade down conductor 9 leading to a rotor-blade-side conductive slideway 17".
  • the rotor blades 5 are made of electrically non-conducting material, such as glass-fiber-reinforced plastics, at least in the root section of the blades, so that electric charges on a rotor blade 5 cannot be discharged towards the hub 4 via the rotor-blade 5 itself.
  • the rotor blades 5 can be pitched, i.e. the aerodynamic angle-of-attack can be adjusted by rotating the blades 5 around their longitudinal axes, by means of a pitch bearing 11 located between the rotor-blade root and the hub 4 (Fig. 4).
  • the hub 4 is mounted on a main shaft 10, supported by main-shaft bearings in the nacelle 3 (Fig. 4).
  • the wind turbine 1 is equipped with a grounding system that includes a rotor-blade discharge unit 13 for each rotor blade 5.
  • the grounding system prevents the rotor blades 5 from becoming charged up with static charges, and protects the mechanical and electronic equipment from damage caused by lightning strikes.
  • the tip parts 8 of rotor blades 5 are equipped with lightning receptors 6 electrically connected to rotor blade down conductors 9 leading internally along the rotor blades 5.
  • further lightning receptors are distributed over the length of the rotor blades 5 and are connected to rotor blade down conductors 9.
  • the light- ning receptors, which are distributed along the rotor blades 5, may not only be struck by lightning, but also collect static charges
  • the blades 5 are equipped with devices to accept lightning strikes, which are connected to the rotor blade down conductors 9, designed to collect electric charges created by the rotation of the rotor blades 5.
  • the rotor blade down conductors 9 transfer electric charges from the tip parts 8 to the rotor-blade-side conductive slideways 17" located at the roots of the rotor blades 5.
  • Each rotor-blade-side conductive slideway 17" has an electrical connection to a roller device 15, 16 as shown in Fig. 2 and Fig. 3.
  • Each rotor-blade discharge unit 13 has an electrical connection to the grounded nacelle 3, therefore the tip parts 8 are electrically connected to a ground potential 12. Hence, the wind turbine 1 is grounded.
  • the roller device 15 shown in Fig. 2 is part of an exemplary current transfer arrangement 50 and has two contact wheels 30A and 30B, which are arranged to roll along a conductive slideway 17.
  • the contact wheels 30A, 30B are rotatably mounted on the chassis 32 by a front axle 37A and a rear axle 37B, respectively.
  • the chassis 32 is made of conductive material, e.g. steel, and is spaced from the conductive slideway 17 by the contact wheels 30A, 30B.
  • a discharge cable 19 is electrically connected to the chassis 32 of roller device 15.
  • the roller device 15 is biased towards the conductive slideway 17, as shown in Fig. 7.
  • the contact wheels 30A, 30B are made of a material that deforms due to the elastic bias acting on the chassis 32 and an electrical connection of the contact wheels 30A, 30B to the conductive slideway 17 is thereby ensured because of the increased contact area of the wheels. If the galvanic connection was lost, static discharges between the conductive slideway 17 and the roller device 15 would occur, leading to spark erosions of the current transfer arrangement 50. In the event of lightning striking a rotor blade 5 an arc will form between the con- ductive slideway 17 that is electrically connected to the rotor blades and the chassis 32 acting as a spark-gap electrode. The arc will form across a spark gap 33.
  • the lightning current will not pass through the contact wheels 30A, 30B due to their resistivity.
  • the voltage drop across the contact wheels 30A, 30B is so high that flashover will occur between the chassis 32 and the conductive slideway 17.
  • the contact wheels 30A, 30B as well as the wheel and axle bearings are not exposed to the full lightning current.
  • the exemplary roller device 16 illustrated in Fig. 3 is part of a current transfer arrangement 60.
  • This roller device 16 is identical to the roller device 15, described in accordance with Fig. 2, and differs from roller device 15 only in one feature.
  • the chassis 42 of roller device 16 exhibits a protrusion 34 on the surface of chassis 42 that faces the conductive slideway 17. This protrusion 34 acts as the spark-gap electrode of roller device 16.
  • a hub region including a rotor-blade discharge unit 13 associated with each rotor blade 5 is illustrated in more detail in Fig. 4.
  • the pitch bearing 11 is mounted on the hub 4, which, in turn, is fixedly mounted on the main shaft 10.
  • the root part of a rotor blade 5 is mounted on the associated pitch bearing 11 and is equipped with a rotor-blade-side conductive slideway 17".
  • This conductive slideway 17" is associated with a current transfer arrangement 50" (Fig. 7) and is electrically connected to a rotor blade down conductor 9.
  • the rotor-blade discharge unit 13, shown in Fig. 4 establishes an electrical connection between the rotor-blade-side conductive slideway and the nacelle-side conductive slideway 17' that is electrically connected to a conductor 40, e.g. a cable, which in turn is connected to the ground 12.
  • the main shaft 10 rotates around a nearly horizontal axis, whereas the rotor blades 5 are ro- tatable around nearly longitudinal axes which are perpendicular to the main-shaft axis.
  • the rotor blade 5 and the nacelle 3 rotate around two perpendicular axes if the pitch angle of the rotor blade 5 is altered with respect to the hub.
  • the rotor-blade discharge units 13 are fixedly mounted on the hub 4, and the hub 4 is fixedly mounted on the main shaft 10, the rotor-blade discharge units 13 rotate with the main shaft 10.
  • the exemplary rotor-blade discharge unit 13 including roller device 15", shown in Fig.
  • the roller device 15" is part of a current transfer arrangement 50" associated with the rotor blade 5, the current transfer arrangement 50" together with the associated electrical connection to the hub 4 via discharge cable 19A make up the rotor-blade discharge unit 13.
  • the rotor blade 5 has a ro- tor-blade-side conductive slideway 17" that is arranged around the root of the rotor blade 5, as already described in conjunction with Fig. 4.
  • the roller-device 15" enables charges to be transferred from the rotor-blade-side slideway 17" to the hub 4, thereby bypassing the pitch bearing 11 .
  • the rotor-blade-side conductive slideway 17" is internally connected to the rotor blade down conductor 9.
  • the rotor blade 5 is made of non-conductive material in this ex- emplary embodiment, there is no direct electric path between the rotor-blade-side conductive slideway 17" and the hub 4.
  • the only electrical connection between a rotor blade 5 and the hub 4 is provided by the rotor-blade discharge unit 13.
  • front and rear axles 37A and 37B of roller device 15" on which the contact wheels 30A, 30B of roller device 15" are mounted, as shown in Fig. 2, line up.
  • a projection of axles 37A and 37B is depicted in Fig. 5 as a dashed line 37".
  • the roller device 15" is mounted at one end of a bendable strip 24 which at its opposite end is fixedly mounted in an electrically insulated manner by mounting bolts 22 on an immobile part of the pitch bearing 11 .
  • the bendable strip 24 is bent in such a way that it elastically bi- ases the contact wheels 30A, 30B of roller device 15" (shown in Fig. 2 in more detail) towards the rotor-blade-side conductive slideway 17".
  • the further exemplary embodiment of the rotor-blade discharge unit 13 shown in Fig. 6 includes the roller device 15', which is depicted in more detail in Fig. 2.
  • the rotor-blade dis- charge unit 13 is mounted on the hub 4 between the root of rotor blade 5 and the nacelle 3.
  • the roller device 15' enables charges to be transferred directly from a rotor blade down conductor 9 to a nacelle-side slideway 17', which is electrically connected to a structural part of the nacelle 3 by a conductor 40, for example, a cable.
  • the whole structural part of the nacelle 3 is used for conducting the lightning current to the tower 2.
  • the rotor blades 5 are made of non-conductive material, there is no electrical path between the rotor blade 5 and the hub 4.
  • the rotor-blade discharge unit 13 is formed by the current transfer arrangement 50' including the nacelle-side conductive slideway 17'.
  • the roll- er device 15' is electrically connected to the rotor blade down conductor 9 over a discharge- cable 19B.
  • the roller device 15' is biased towards the nacelle-side conductive slideway 17' and therefore the wheels 30A, 30B of roller device 15' form a contact surface with the nacelle-side conductive slideway 17'.
  • axles 37A, 37B of roller device 15' on which the contact wheels 30A, 30B of roller device 15' are mounted, as shown in Fig. 2, line up.
  • a projection of axles 37A and 37B is depicted in Fig. 6 as a dashed line 37'.
  • the roller device 15' is mounted at one end of an elastically deformable strip 23 which at its opposite end is fixedly mounted in an electrically insulated manner by mounting bolts 22 on an immobile part of the pitch bearing 11 .
  • the bendable strip 23 is bent in such a way that it elastically biases the contact wheels 30A, 30B of the roller device 15' (shown in Fig. 2 in more detail) towards the nacelle-side conductive slideway 17'.
  • a rotor-blade discharge unit 13 for each rotor blade 5 is provided.
  • the nacelle-side conductive slideway 17' is therefore shared between three current transfer arrangements 50'.
  • FIG. 7 Another exemplary embodiment of the rotor-blade discharge unit 13 is illustrated in Fig. 7.
  • the rotor-blade discharge unit 13 is mounted on the hub 4 between the root of a rotor blade 5 and the nacelle 3.
  • Each rotor blade 5 has a rotor-blade-side conductive slideway 17", associated with current transfer arrangement 50" that is arranged around the root of the rotor blade 5 and is internally connected to the rotor blade down conductor 9.
  • the surface of nacelle 3 facing the hub 4 provides the nacelle-side conductive slideway 17', associated with current transfer arrangement 50'.
  • This nacelle-side conductive slideway 17' is arranged around a main-shaft opening of the nacelle 3, which is electrically coupled to the grounded part(s) of the nacelle 3 by a conductor 40.
  • roller devices 15', 15" are biased to the nacelle-side conductive slideway 17' or the rotor- blade-side conductive slideway 17", respectively. Thereby enabling charges to be transferred directly from the rotor-blade-side conductive slideway 17" to the nacelle-side conductive slideway 17', while bypassing the hub 4, as they are electrically connected by discharge cable 19C. Since in this exemplary embodiment each rotor blade 5 is made of non-conducting material, there is no direct electrical path between the rotor-blade-side conductive slideway 17" and the hub 4.
  • the rotor-blade discharge unit 13 is formed by two current transfer ar- rangements 50', 50", including roller devices 15', 15" contacting the rotor-blade-side conductive slideway 17" and the nacelle-side conductive slideway 17', respectively.
  • front and rear axles 37A, 37B of roller devices 15', 15" which are shown in Fig. 2 for each roller device 15 individually, on which the contact wheels 30A, 30B of roller devices 15', 15" are mounted, line up for each roller device 15', 15", respectively.
  • a projection of front and rear axles 37A, 37B of roller devices 15', 15" is depicted by dashed lines 37', 37" in Fig. 7, for the roller devices 15', 15".
  • roller device 15' is mounted at one end of the bendable strip 23 which at its opposite end is fixedly mounted in an electrically insulated manner by mounting bolts 22, on an immobile part of the pitch bearing 11 .
  • the bendable strip 23 is bent in such a way that it elastically biases the roller device 15' towards the nacelle-side conductive slideway 17'.
  • roller device 15" is mounted at one end of the bendable strip 24, which is mounted on the pitch bearing 11 in the same way as bendable strip 23.
  • the elastically deformable strip 24 is bent such that it elastically biases the roller device 15" towards the rotor-blade-side conductive slideway 17".
  • the chassis 32 of roller devices 15' and 15" are electrically coupled via the discharge-cable 19C, thereby providing a current path from the rotor-blade side conductive slideway 17" to the nacelle-side conductive slideway 17'.
  • the nacelle-side conductive slideway 17' is shared between three current transfer arrangements 50'.

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  • Engineering & Computer Science (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Sustainable Development (AREA)
  • Sustainable Energy (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Wind Motors (AREA)

Abstract

La présente invention concerne une unité de décharge de pale de rotor permettant de décharger des charges électriques d'une pale de rotor d'une éolienne, l'unité de décharge de pale de rotor comprenant au moins un agencement de transfert de courant, l'agencement de transfert de courant comprenant : un dispositif à galets, une glissière électroconductrice, un éclateur, le dispositif à galets étant sollicité vers la glissière conductrice et étant mobile par rapport à la glissière conductrice, le dispositif à galets comprenant : au moins une roue de contact, ayant une surface de roulement et la roue de contact étant conçue pour rouler sur la glissière conductrice et étant sollicitée vers la glissière conductrice, la surface de roulement étant conçue pour se déformer contre la glissière conductrice sous l'effet de la sollicitation agissant sur le dispositif à galets, la roue de contact et la glissière conductrice formant un premier trajet de courant destiné à décharger les charges électriques et l'éclateur formant un second trajet de courant lors de l'apparition d'une étincelle pontant l'éclateur, le second trajet de courant étant connecté en parallèle audit premier trajet de courant.
EP14811760.9A 2013-12-09 2014-12-08 Unité de décharge de pale de rotor pour éoliennes Active EP3080447B1 (fr)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
GB201321695A GB201321695D0 (en) 2013-12-09 2013-12-09 Lighting current transfer arrangement of a wind turbine
DKPA201470241 2014-04-25
PCT/DK2014/050418 WO2015086025A1 (fr) 2013-12-09 2014-12-08 Unité de décharge de pale de rotor pour éoliennes

Publications (2)

Publication Number Publication Date
EP3080447A1 true EP3080447A1 (fr) 2016-10-19
EP3080447B1 EP3080447B1 (fr) 2019-06-12

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Family Applications (1)

Application Number Title Priority Date Filing Date
EP14811760.9A Active EP3080447B1 (fr) 2013-12-09 2014-12-08 Unité de décharge de pale de rotor pour éoliennes

Country Status (3)

Country Link
EP (1) EP3080447B1 (fr)
DK (1) DK3080447T3 (fr)
WO (1) WO2015086025A1 (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3726051A1 (fr) * 2019-04-17 2020-10-21 Siemens Gamesa Renewable Energy A/S Dispositif de connexion électrique d'une éolienne, éolienne et procédé de fabrication d'un dispositif de connexion électrique

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ES2731173B2 (es) 2018-05-14 2020-12-09 Siemens Gamesa Renewable Energy Innovation & Technology SL Sistema de protección eléctrica para aerogeneradores
EP3708829B1 (fr) * 2019-03-11 2023-09-06 Siemens Gamesa Renewable Energy Innovation & Technology, S.L. Système de protection contre la foudre pour une éolienne et éolienne comprenant un tel système de protection contre la foudre
EP3744972B1 (fr) * 2019-05-27 2023-01-11 Siemens Gamesa Renewable Energy A/S Rotor d'éolienne et éolienne

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DK177270B1 (da) * 2002-11-12 2012-09-10 Lm Wind Power As Lynbeskyttelse af pitchreguleret vindmøllevinge
US7654790B2 (en) * 2003-11-20 2010-02-02 Vestas Wind Systems A/S Wind turbine lightning connection means method and use hereof
DE102004012946B4 (de) * 2004-03-17 2006-03-23 Stemmann-Technik Gmbh Windenergieanlage
EP2336560A1 (fr) * 2009-12-15 2011-06-22 Vestas Wind Systems A/S Ensemble de transfert de courant d'éclairage pour éolienne
WO2012016726A2 (fr) * 2010-08-02 2012-02-09 Vestas Wind Systems A/S Agencement de transfert d'un courant de foudre d'une éolienne

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3726051A1 (fr) * 2019-04-17 2020-10-21 Siemens Gamesa Renewable Energy A/S Dispositif de connexion électrique d'une éolienne, éolienne et procédé de fabrication d'un dispositif de connexion électrique
WO2020212043A1 (fr) * 2019-04-17 2020-10-22 Siemens Gamesa Renewable Energy A/S Dispositif de connexion électrique pour une éolienne, éolienne et procédé de fabrication d'un dispositif de connexion électrique

Also Published As

Publication number Publication date
EP3080447B1 (fr) 2019-06-12
WO2015086025A1 (fr) 2015-06-18
DK3080447T3 (da) 2019-07-22

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